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Glenn Research Center
Aircraft Operations 1
GRC Aircraft Operations Office
National Aeronautics and Space Administration
www.nasa.gov 2
Mission
• Provide safety, operational, and engineering oversight to
all GRC research experiments involving flight, including
non-NASA controlled aircraft/UAS.
• Manage, operate, and maintain GRC based research and
research support aircraft/UAS.
• Manage the operation and maintenance of the GRC
Hangar and associated systems and equipment.
• Provide support for transient aircraft/UAS, including
NASA, military, civilian, and other Government agencies.
National Aeronautics and Space Administration
www.nasa.gov
Flight Operations Staff
Staff Capability
–Pilots
–Engineering
• Mechanical
• Electrical
–Maintenance
–Fabrication
• Electrical
• Mechanical
Panel 6-7Panel 5-6
Panel 4-5
Panel 3-4
Panel 2-3
Panel 1-21 2
3
4
5
678
9
10
11
12
National Aeronautics and Space Administration
www.nasa.gov
NASA Glenn Aircraft Operations
•Twin Otter DHC-6 Learjet 25
S-3B Viking T-34C Turbo-Mentor
National Aeronautics and Space Administration
www.nasa.gov
Learjet Model 25 Right Side
IR Quartz Window Available
Inside Right Windows
Inside Right Window Close Up
9.75” X 10.5” Opening Starboard Instrument Pod
National Aeronautics and Space Administration
www.nasa.gov
Learjet Model 25 Left Side Photos
Motorized Sliding Door
Left Window and Overhead Ports/Mounts
13.5” X 10.5” Opening
Door Operational in Flight
Left Windows
National Aeronautics and Space Administration
www.nasa.gov
Learjet Model 25 Viewports
12” Diameter Openings
Close Up of View Port/Instrument Mount
National Aeronautics and Space Administration
www.nasa.gov
Learjet Model 25 Right Side Fuselage Pod
View Port/Instrument Mount 22” X 19”
View Port/Mount From the Inside
Second Pod Available on Door Side
Cabin Access to Viewport/Instrument Mount
National Aeronautics and Space Administration
www.nasa.gov
Learjet 25 Great Lakes Environmental Mission
National Aeronautics and Space Administration
www.nasa.gov
Learjet 25 CO2 Sounder
National Aeronautics and Space Administration
www.nasa.gov 11
CO2 Sounder/ NASA Glenn Lear-25 ARM Site Field Deployment
Photos from DOE ARM Site deployment:
Background - NASA Glenn Lear 25 takeoff from
Ponca City Airport on 12/7/08 (Graham Allan photo)
Left- Goddard field experiment team
Right - DOE Cessna aircraft with in-situ CO2
sampling equipment
National Aeronautics and Space Administration
www.nasa.gov 12
An initial Plot of the airborne flight patterns above the ARM site
from airborne GPS data and Google Earth
National Aeronautics and Space Administration
www.nasa.gov
Learjet 25 Solar Cell Calibration
National Aeronautics and Space Administration
www.nasa.gov
Learjet 25 Microgravity
National Aeronautics and Space Administration
www.nasa.gov
NASA Glenn Research Center
S-3B Viking Aircraft
National Aeronautics and Space Administration
www.nasa.gov
S-3B Viking Research Capabilities
• The NASA S-3B Viking aircraft is a highly modified version of the Lockheed-Martin
S-3B aircraft which flew operationally in the U.S. Navy for more than 30 years. Originally
designed for the carrier-based anti-submarine warfare mission, the aircraft utilizes two fuel
efficient General Electric TF34 turbofan engines enabling long range and mission
endurance. The NASA S-3B is capable of carrying a wide variety of research sensors and
equipment either internally or in a pod-mounted configuration on either of two wing pylons.
The aircraft features a modern avionics suite and state-of-the-art research stations to
accommodate two inflight researchers in addition to the two pilots. An installed Inmarsat
BGAN (Broadband Global Area Network) system brings with it the capability to transmit
voice and data in real time from the aircraft to ground stations providing seamless network
coverage across most of the world's landmass.
National Aeronautics and Space Administration
www.nasa.gov
• S-3B FLIGHT ENVELOPE
• ALTITUDE: Surface to 40,000 ft msl
• AIRSPEED: 100 - 450 KIAS (0.79m limit)
• ENDURANCE: Up to 7 hours with external fuel tanks, 5 hours with internal fuel only
• RANGE: Up to 2500 nm with external fuel tanks, 1800 miles with internal fuel only
• G-LIMITS: + 3.5 to - 1.0 g
• PAYLOAD: Up to 2500 lbs per wing pylon, Up to 4000 lbs in bomb bay
• GROSS WT: Max takeoff gross weight of 52500 lbs, empty weight approximately 27500 lbs
• CREW: 2 pilots + 2 researchers
• COMM: VHF, UHF, SATCOM (INMARSAT BGAN - Broadband Global Area Network)
• NAV: Military GPS/INS and Commercial GPS (WAAS)
S-3B Viking Research Capabilities
National Aeronautics and Space Administration
www.nasa.gov
Electrical Capacity
115 Volts AC 60 Hz: 14 KVA
115 Volts AC 400 Hz: 200 amps
28 Volts DC: 600 amps
External Capacity
2 Wing Mounts
Two (2) External Sensor Pods
Two (2) Heated Bomb Bays
Approximately 28” width, 90” length, 25” high
Aft Sensor Area
Internal Capacity Avionics Bay
Approximately 75” width, 90” length, 36” high
S-3B Viking Research Capabilities
National Aeronautics and Space Administration
www.nasa.gov
Electrical Capacity
115 Volts AC 60 Hz: 14 KVA
115 Volts AC 400 Hz: 200 amps
28 Volts DC: 600amps
External Capacity
2 Wing Mounts
Two (2) External Sensor Pods
Two (2) Heated Bomb Bays
Approximately 28” width, 90” length, 25” high
Aft Sensor Area
Internal Capacity Avionics Bay
Approximately 75” width, 90” length, 36” high
S-3B Viking Research Capabilities
Standard Mount – Both wings
National Aeronautics and Space Administration
www.nasa.gov
Electrical Capacity
115 Volts AC 60 Hz: 14 KVA
115 Volts AC 400 Hz: 200 amps
28 Volts DC: 600amps
External Capacity
2 Wing Mounts
Two (2) External Sensor Pods
Two (2) Heated Bomb Bays
Approximately 28” width, 90” length, 25” high
Aft Sensor Area
Internal Capacity Avionics Bay
Approximately 75” width, 90” length, 36” high
S-3B Viking Research Capabilities
External Cargo Pod
Floor Stanchions with
Restraint Panels
Two (2) Nets or Lateral
Straps at 10 in. Max
Spacing (Door Area
Only)
National Aeronautics and Space Administration
www.nasa.gov
Cargo pod that has been
previously modified for
use by NRL/NOAA on P-3
aircraft
GRC has four cargo pods
available for modification
as desired to support future
research requirements
S-3B Viking Research Capabilities
NADIR port
National Aeronautics and Space Administration
www.nasa.gov
Electrical Capacity
115 Volts AC 60 Hz: 14 KVA
115 Volts AC 400 Hz: 200 amps
28 Volts DC: 600amps
External Capacity
2 Wing Mounts
Two (2) External Sensor Pods
Two (2) Heated Bomb Bays
Approximately 28” width, 90” length, 25” high
Aft Sensor Area
Internal Capacity Avionics Bay
Approximately 75” width, 90” length, 36” high
S-3B Viking Research Capabilities
Aft Sensor Area (Tubes depicted are removable) Heated Bomb Bay
National Aeronautics and Space Administration
www.nasa.gov
S-3B Viking Research Capabilities
Electrical Capacity
115 Volts AC 60 Hz: 14 KVA
115 Volts AC 400 Hz: 200 amps
28 Volts DC: 600amps
External Capacity
2 Wing Mounts
Two (2) External Sensor Pods
Two (2) Heated Bomb Bays
Approximately 28” width, 90” length, 25” high
Aft Sensor Area
Internal Capacity Avionics Bay
Approximately 75” width, 90” length, 36” high Small Instrument/Sensor Location
National Aeronautics and Space Administration
www.nasa.gov
S-3B Viking Research Capabilities
Electrical Capacity
115 Volts AC 60 Hz: 14 KVA
115 Volts AC 400 Hz: 200 amps
28 Volts DC: 600amps
External Capacity
2 Wing Mounts
Two (2) External Sensor Pods
Two (2) Heated Bomb Bays
Approximately 28” width, 90” length, 25” high
Aft Sensor Area
Internal Capacity Avionics Bay
Approximately 75” width, 90” length, 36” high
Avionics Bay – Aft Cabin Area
National Aeronautics and Space Administration
www.nasa.gov
MAST Pod Overview Multi-Mission Advanced Sensor Testbed
• Length: 153.8”
• Width: 25.71”
• Weight: 517 lb. (including sensor payload)
• Aircraft Interface: – 14” or 30” MIL STD wing store suspension
– MIL STD power, data, and video connections
• Core components: – Argon ST 14” Aeroscout gimbal with VNIR hyper
spectral imaging system
– Argon ST Common Data Acquisition System (CDAS)
– C-MIGITS GPS/INS navigation suite (sub-meter accuracy)
– Gigabit ethernet switched network
– 28VDC filtered power supply
– L band video transmitter (ROVER compatible)
– 19” vibration isolated racks (forward and aft)
– Center nadir imaging bay
• Optional components: – Argon ST Daedelus Airborne Multispectral
Scanner (AMS) – installed in nadir bay
• Extensibility/Modularity: – Gigabit ethernet and CDAS provide a backbone
command/control and data collection system for installed payloads
– Mission-tailored, gimbal-installed hyper spectral cameras
– Adaptable nose and tail bays support a wide array of imaging, radar, or antenna payloads
– Center nadir bay
– Significant size, weight, and power (SWAP) margins for additional research system installation
UNCLASS – Copyright 2009, Argon ST Inc.
National Aeronautics and Space Administration
www.nasa.gov UNCLASS – Copyright 2009, Argon ST Inc.
S-3B Multi-Mission Advanced Sensor Testbed
(MAST)
National Aeronautics and Space Administration
www.nasa.gov
Twin Otter DHC-6 Research Capabilities
Electrical Capacity
115 Volts AC 60 Hz: 16 amps
115 Volts AC 400 Hz: 35 amps
28 Volts DC: 80 amps
External Capacity Five (5) External Hard Wing Mounts +
Various Small Instrument Mounts
Internal Capacity
Three (3) Internal Research Hardware Locations
Front Section, Main Fuselage, Rear Fuselage
Overhead Hatch
Picture Window
Picture Window
Inside View of Overhead Hatch Outside View of Overhead Hatch 18” X 17.25”
National Aeronautics and Space Administration
www.nasa.gov
Twin Otter DHC-6 Research Capabilities
Electrical Capacity
115 Volts AC 60 Hz: 16 amps
115 Volts AC 400 Hz: 35 amps
28 Volts DC: 80 amps
External Capacity Five (5) External Hard Wing Mounts +
Various Small Instrument Mounts
Internal Capacity
Three (3) Internal Research Hardware Locations
Front Section, Main Fuselage, Rear Fuselage
Overhead Hatch
Picture Window
49” x 48” Plexiglas opening (3/4” thick)
National Aeronautics and Space Administration
www.nasa.gov
Twin Otter DHC-6 Research Capabilities
Current Installation – Looking Forward
Rack #1 Video Suite Rack #2 Data Acquisition
Standard Racks Reconfigured to Meet Customer
Needs
National Aeronautics and Space Administration
www.nasa.gov
T-34C Mentor Research Capabilities
Sensor Installed on Door Panel
Close Up View
National Aeronautics and Space Administration
www.nasa.gov
T-34C Mentor Research Capabilities
Small Research Location
Fuselage Research Pod
National Aeronautics and Space Administration
www.nasa.gov
NASA Glenn Research Center
Aircraft Operations
Points of Contact
Alan J. Micklewright, Chief of Aircraft Operations
Phone: 216-433-2036
Ed Emery, Experiments Manager
Phone: 216-433-5694